JPH0320048B2 - - Google Patents
Info
- Publication number
- JPH0320048B2 JPH0320048B2 JP58092238A JP9223883A JPH0320048B2 JP H0320048 B2 JPH0320048 B2 JP H0320048B2 JP 58092238 A JP58092238 A JP 58092238A JP 9223883 A JP9223883 A JP 9223883A JP H0320048 B2 JPH0320048 B2 JP H0320048B2
- Authority
- JP
- Japan
- Prior art keywords
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- composition
- permanent magnet
- sintering
- temperature
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 239000000463 material Substances 0.000 claims description 69
- 239000000203 mixture Substances 0.000 claims description 38
- 238000005245 sintering Methods 0.000 claims description 36
- 229910045601 alloy Inorganic materials 0.000 claims description 33
- 239000000956 alloy Substances 0.000 claims description 33
- 238000004519 manufacturing process Methods 0.000 claims description 31
- 229910052761 rare earth metal Inorganic materials 0.000 claims description 25
- 239000000843 powder Substances 0.000 claims description 20
- 238000000465 moulding Methods 0.000 claims description 13
- 239000002245 particle Substances 0.000 claims description 13
- 239000000654 additive Substances 0.000 claims description 10
- 230000000996 additive effect Effects 0.000 claims description 10
- 238000010438 heat treatment Methods 0.000 claims description 9
- 229910052804 chromium Inorganic materials 0.000 claims description 4
- 229910052721 tungsten Inorganic materials 0.000 claims description 4
- 230000032683 aging Effects 0.000 description 27
- 238000011282 treatment Methods 0.000 description 27
- XEEYBQQBJWHFJM-UHFFFAOYSA-N iron Substances [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 22
- 239000012298 atmosphere Substances 0.000 description 13
- 238000001816 cooling Methods 0.000 description 12
- 238000000034 method Methods 0.000 description 12
- 229910052779 Neodymium Inorganic materials 0.000 description 11
- 229910052777 Praseodymium Inorganic materials 0.000 description 10
- 150000002910 rare earth metals Chemical class 0.000 description 10
- 229910052796 boron Inorganic materials 0.000 description 9
- 230000007423 decrease Effects 0.000 description 9
- 230000000694 effects Effects 0.000 description 8
- 230000004907 flux Effects 0.000 description 7
- 229910001047 Hard ferrite Inorganic materials 0.000 description 6
- YXFVVABEGXRONW-UHFFFAOYSA-N Toluene Chemical compound CC1=CC=CC=C1 YXFVVABEGXRONW-UHFFFAOYSA-N 0.000 description 6
- 239000012535 impurity Substances 0.000 description 6
- 239000011261 inert gas Substances 0.000 description 6
- 229910052782 aluminium Inorganic materials 0.000 description 5
- 229910052799 carbon Inorganic materials 0.000 description 5
- 150000001875 compounds Chemical class 0.000 description 5
- 239000013078 crystal Substances 0.000 description 5
- 230000005347 demagnetization Effects 0.000 description 5
- 239000007789 gas Substances 0.000 description 5
- 229910052760 oxygen Inorganic materials 0.000 description 5
- 229910052710 silicon Inorganic materials 0.000 description 5
- 239000010409 thin film Substances 0.000 description 5
- 229910052791 calcium Inorganic materials 0.000 description 4
- 229910017052 cobalt Inorganic materials 0.000 description 4
- 239000010941 cobalt Substances 0.000 description 4
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 4
- 230000000052 comparative effect Effects 0.000 description 4
- 229910052802 copper Inorganic materials 0.000 description 4
- 239000010949 copper Substances 0.000 description 4
- 229910052742 iron Inorganic materials 0.000 description 4
- 229910052749 magnesium Inorganic materials 0.000 description 4
- 230000005415 magnetization Effects 0.000 description 4
- 230000001590 oxidative effect Effects 0.000 description 4
- 238000010298 pulverizing process Methods 0.000 description 4
- 238000010791 quenching Methods 0.000 description 4
- 239000002994 raw material Substances 0.000 description 4
- 238000004544 sputter deposition Methods 0.000 description 4
- 229910052772 Samarium Inorganic materials 0.000 description 3
- 238000007796 conventional method Methods 0.000 description 3
- 239000000696 magnetic material Substances 0.000 description 3
- VLKZOEOYAKHREP-UHFFFAOYSA-N n-Hexane Chemical compound CCCCCC VLKZOEOYAKHREP-UHFFFAOYSA-N 0.000 description 3
- 239000003960 organic solvent Substances 0.000 description 3
- 229910052698 phosphorus Inorganic materials 0.000 description 3
- 238000003825 pressing Methods 0.000 description 3
- 239000002904 solvent Substances 0.000 description 3
- 238000006467 substitution reaction Methods 0.000 description 3
- CSCPPACGZOOCGX-UHFFFAOYSA-N Acetone Chemical compound CC(C)=O CSCPPACGZOOCGX-UHFFFAOYSA-N 0.000 description 2
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 2
- 229910052684 Cerium Inorganic materials 0.000 description 2
- 229910052692 Dysprosium Inorganic materials 0.000 description 2
- 229910052691 Erbium Inorganic materials 0.000 description 2
- 229910052693 Europium Inorganic materials 0.000 description 2
- 229910052688 Gadolinium Inorganic materials 0.000 description 2
- 229910052765 Lutetium Inorganic materials 0.000 description 2
- 229910052775 Thulium Inorganic materials 0.000 description 2
- 229910052769 Ytterbium Inorganic materials 0.000 description 2
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 2
- 239000011230 binding agent Substances 0.000 description 2
- 238000005260 corrosion Methods 0.000 description 2
- 230000007797 corrosion Effects 0.000 description 2
- 230000002431 foraging effect Effects 0.000 description 2
- 230000006872 improvement Effects 0.000 description 2
- 238000009776 industrial production Methods 0.000 description 2
- 239000000314 lubricant Substances 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- 229910052758 niobium Inorganic materials 0.000 description 2
- 230000003647 oxidation Effects 0.000 description 2
- 238000007254 oxidation reaction Methods 0.000 description 2
- 239000001301 oxygen Substances 0.000 description 2
- 238000004663 powder metallurgy Methods 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 238000012545 processing Methods 0.000 description 2
- 230000001737 promoting effect Effects 0.000 description 2
- 239000007858 starting material Substances 0.000 description 2
- 229910052717 sulfur Inorganic materials 0.000 description 2
- 229910052720 vanadium Inorganic materials 0.000 description 2
- 229910052727 yttrium Inorganic materials 0.000 description 2
- UOCLXMDMGBRAIB-UHFFFAOYSA-N 1,1,1-trichloroethane Chemical compound CC(Cl)(Cl)Cl UOCLXMDMGBRAIB-UHFFFAOYSA-N 0.000 description 1
- 229910000758 Br alloy Inorganic materials 0.000 description 1
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 229910000640 Fe alloy Inorganic materials 0.000 description 1
- 229910000604 Ferrochrome Inorganic materials 0.000 description 1
- YCKRFDGAMUMZLT-UHFFFAOYSA-N Fluorine atom Chemical compound [F] YCKRFDGAMUMZLT-UHFFFAOYSA-N 0.000 description 1
- 229910052689 Holmium Inorganic materials 0.000 description 1
- 229910000846 In alloy Inorganic materials 0.000 description 1
- CTQNGGLPUBDAKN-UHFFFAOYSA-N O-Xylene Chemical compound CC1=CC=CC=C1C CTQNGGLPUBDAKN-UHFFFAOYSA-N 0.000 description 1
- 229910052771 Terbium Inorganic materials 0.000 description 1
- XSTXAVWGXDQKEL-UHFFFAOYSA-N Trichloroethylene Chemical group ClC=C(Cl)Cl XSTXAVWGXDQKEL-UHFFFAOYSA-N 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 239000005456 alcohol based solvent Substances 0.000 description 1
- 229910000828 alnico Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- -1 and Co Inorganic materials 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 239000003638 chemical reducing agent Substances 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000002542 deteriorative effect Effects 0.000 description 1
- 239000012776 electronic material Substances 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 239000011737 fluorine Substances 0.000 description 1
- 229910052731 fluorine Inorganic materials 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 229910052746 lanthanum Inorganic materials 0.000 description 1
- 229910001004 magnetic alloy Inorganic materials 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 239000012188 paraffin wax Substances 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 230000001568 sexual effect Effects 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
- 229910052715 tantalum Inorganic materials 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- UBOXGVDOUJQMTN-UHFFFAOYSA-N trichloroethylene Natural products ClCC(Cl)Cl UBOXGVDOUJQMTN-UHFFFAOYSA-N 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- 239000008096 xylene Substances 0.000 description 1
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01F—MAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
- H01F1/00—Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties
- H01F1/01—Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials
- H01F1/03—Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity
- H01F1/032—Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity of hard-magnetic materials
- H01F1/04—Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity of hard-magnetic materials metals or alloys
- H01F1/06—Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity of hard-magnetic materials metals or alloys in the form of particles, e.g. powder
- H01F1/08—Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity of hard-magnetic materials metals or alloys in the form of particles, e.g. powder pressed, sintered, or bound together
- H01F1/086—Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity of hard-magnetic materials metals or alloys in the form of particles, e.g. powder pressed, sintered, or bound together sintered
Landscapes
- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Powder Metallurgy (AREA)
- Hard Magnetic Materials (AREA)
Description
本発明は新規な希土類磁石材料の製造方法に係
り、FeBRを基礎として添加元素Mを含み特に
Smなどの希少希土類金属を必ずしも必要とせず
資源的に豊富でかつ用途が少ないNdやPrを中心
とする軽希土類とFeを主成分とする高性能な永
久磁石材料の製造方法に関する。
永久磁石材料は一般家庭の各種電気製品から大
型コンピユーターの周辺端末機器まで幅広い分野
で使用されている極めて重要な電気・電子材料の
一つである。近年電気機器の小型化、高効率化の
要求にともない、永久磁石材料はますます高性能
化が求められている。また実用的にはモーター用
発電機用磁気カツプリング用など極めて大きい逆
磁界のかかる用途も多く高保磁力を有する磁石材
料も求められている。
現在使用されている永久磁石材料のうち代表的
なものはアルニコ、ハードフエライト、および希
土類コバルト磁石材料である。最近の高い磁石特
性を満たす永久磁石材料としては希土類コバルト
磁石材料である。しかし希土類コバルト磁石材料
は資源的に希少なSmを必要とし供給が不安定な
Coを多量に使用するため非常に高価である。
希土類磁石材料がもつと広い分野でかつ多量に
使用されるようになるためには高価なコバルトを
多量に含まず希土類金属として鉱石中に多量に含
まれている軽希土類を主成分とすることが必要で
ある。そのような永久磁石材料への一つの試みと
してRFe2系化合物(但しRは希土類金属の少な
くとも1個)が提案された。クラーク(A.E.
Clark)はスパツタリングにより得られた非晶質
TbFe2は4.2〓で29.5MGOeのエネルギー積をも
ち、これを300〜500℃で熱処理すると室温で保磁
力は3.4KOe、最大エネルギー積は7MGOeを示す
ことを見い出した。同様な研究はSmFe2につい
ても行われ77〓で9.2MGOeを示すことが報告さ
れている。
しかしこれらのものはどれもスパツタリングに
より作成された薄膜であり一般のスピーカーやモ
ーターに使用できる磁石材料ではない。また
PrFe系合金の超急冷により作製したリボンが
2.8KOeの高保磁力を示すことが報告されている。
さらにクーン等は(Fe.B)0.9Tb0.05La0.05の超急冷
により得られた非晶質リボンを627℃で焼鈍する
と保磁力が9KOeにも達することを見い出した
(Brは5KG)。しかしこの場合磁化曲線の角形性
が悪いため最大エネルギー積は低い(N.C.Koon
他Appl.Phys.Lett.39(10)1981、840〜842頁)。
またカバコフ(L.Kabacoff)等は(Fe、B)1-
XPrX(x=0〜0.3原子比)の組成の超急冷で作成
したリボンはFePr2成分系で室温でKOeレベルの
保磁力をもつものがあると報告している。これら
の超急冷でのリボン又はスパツタリングによる薄
膜はそれ自体として使用可能な実用永久磁石材料
ではなく、これらのリボンや薄膜から実用永久磁
石材料を得ることは出来ない。即ち従来提案され
ているFeBR系のリボン又はRFe系の薄膜からは
任意の形状・寸法を有するバルク永久磁石材料を
得ることは出来ない。又これまでに報告された
FeBr系のリボンの磁化曲線は角形性が悪く従来
慣用されている磁石材料に対抗できる実用永久磁
石材料とはみなされない。更に超急冷でのリボ
ン、スパツタリングによる薄膜はいずれも本質上
等方性であり、これから磁気異方性の実用永久磁
石材料を得ることは事実上不可能であつた。
本発明の目的は従来の欠点を除去したSm等の
希小な希土類を必ずしも用いる必要がなくまた
Co等資源的に問題のある成分を多く含まれない
新規な永久磁石材料を得ることを基本目的とす
る。さらに、本発明は、室温で良好な磁石特性を
有し任意の形状・実用寸法に成形でき、磁化曲線
の角形性が高いものであり、資源的に豊富な軽希
土類元素を有効に使用可能な永久磁石材料を簡便
に得るための製造方法を提供せんとするものであ
る。
本発明者等は先にSm、Coを必ずしも用いる必
要のないFeBR系永久磁石材料を発明した(特願
昭57−145072)。このFeBR系永久磁石材料は、
従来知られているRCo5やR2Co17化合物とは異な
る新しい化合物を基礎とし、特にボロン(B)は、従
来の、たとえば非晶質合金作成時の非晶質促進元
素又は粉末冶金法における焼結促進元素として添
加されるものではなく、このFeBR系永久磁石材
料の実体的内容を構成する磁気的に安定で高い磁
気異方性定数を有するR−Fe−B化合物の必須
構成元素であることを明らかにした(なお、上記
FeBR系永久磁石材料に基づき、適当なミクロ組
織を形成することによつて磁気異方性焼結永久磁
石が得られることも明らかにした)。更に、こう
したFeBR系永久磁石材料が、所定の組成を有す
る平均粒度0.3〜80μmの合金粉末(組成物)を成
形し、非酸化性雰囲気において900〜1200℃で焼
結することによつて製造できることも発明し、別
途出願した(特願昭58−88372)。
本発明者らは前記目的を達成するために更にこ
うしたFeBR三元化合物に基づく結晶質の永久磁
石材料の製造方法について鋭意研究したところ
FeBR系を基礎としFeの一部をCoで置換し、添
加元素M(V、Nb、Ta、Mo、W、Cr、Al)を
含むFeCoBRM系の一定の組成範囲の合金粉末を
成形し、焼結し、更に熱処理することにより磁石
特性、特に保磁力を角形性が著しく優れた永久磁
石材料が得られることを見い出し本願発明に至つ
たものである。
即ち、本発明によれば、原子百分率で8〜30%
のR(但しRはYを包含する希土類元素の少なく
とも1種)、2〜28%のB、所定%以下の添加元
素Mの1種又は2種以上(但しM0%を除き、M
は
V9.5%以下、 Nb12.5%以下、
Ta10.5%以下、 Mo9.5%以下、
W9.5%以下、 Cr8.5%以下、
及びAl9.5%以下であり、
2種以上のMを含む場合M合量は含有するMの
当該各元素のうち最大値を有するものの所定%以
下)、及び残部実質上FeからなるFeBRM系組成
のうちFeの一部を全組成に対して50%以下のCo
(0%を除く)で置換してなるFeCoBRM系組成
を有し、900〜1200℃で焼結してなる焼結体を350
℃以上当該焼結温度以下の温度で熱処理すること
を特徴とするFeCoBRM系永久磁石材料の製造方
法によつて、上記目的を達成できる。熱処理によ
つて、同一組成の焼結体に対し他の磁気特性を劣
化させることなく保磁力の顕著な増大が得られ
る。この点は、例えば希土類元素Rの増加による
保磁力の増大の場合残留磁化の減少をもたらすこ
と(特願昭57−145072号参照)に対比するとその
意義は極めて大きい。所定量のMの存在はこの熱
処理による保磁力増大の効果をさらに高めると共
に、Coの存在により実用上十分高いキユリー点
を実現している。又、このFeCoBRM系組成にさ
らに所定%以下の元素X(Cu3.5%以下、S2.0%以
下、C4.0%以下及びP3.5%以下)の一種又は二種
以上を含有してなるFeCoBRM系組成についても
同様な焼結後の熱処理の効果が達成できる。この
場合、かかる焼結体を前記先願におけるように所
定の組成を有する平均粒度0.3〜80μmの合金粉末
組成物を成形、特に非酸化性雰囲気で焼結するこ
とによつて得ることが好ましい。こうして得られ
る永久磁石材料は、磁気異方性永久磁石材料とし
て特に優れた磁気特性を示す。
本発明製法は、従来法によるFeBR系アモルフ
アスリボンと異なり磁気異法性の永久磁石材料が
得られる点で特徴的であるが、等方性材料も製法
でき従来の等方性永久磁石材料に比して優れたも
のが得られる。以下、まず主として磁気異方性永
久磁石材料を製造する場合を基本として説明す
る。
本発明の永久磁石材料の製法において、FeBR
系磁石用合金粉末組成物においてFeをCoにより
一部置換することにより磁石材料の温度特性を改
善するものであるが更には希土類元素Rとして資
源的に豊富なNdやPrなどの軽希土類を用いて高
い磁気特性を発現させるものである。
一般にFe合金へCoの添加は添加量の増大によ
りキユリー点Tcが上昇するものと下降するもの
があり、一般的に添加効果を予測することは困難
である。本発明においてFeのCoによる置換の結
果Coの置換量の増大に伴いTcは徐々に増大する
ことが明らかとなつた。又磁石材料組成のRの種
類によらず同様な傾向が確認される。Coの置換
量はわずかでもTc増大に有効であり、Coの置換
量により約310〜約750℃の任意のTcをもつ合金
が得られるがCo量は50%(以下%は合金中の原
子百分率を示す)以下で十分効果が得られる。
Bは保磁力が1kOe以上を満たすために2%以
上とし、ハードフエライトの残留磁束密度Br約
4kG以上とするためには28%以下である。希土類
元素Rは保磁力1kOe以上とするため8%以上必
要であり、また燃え易く工業的取扱・製造上の困
難のため、また高価であることから30%以下とす
る。Bとしては純ボロン又はハフエロボロンを用
いることが出来、不純物としてAl、Si、Cなど
を含むものを用いることが出来る。
Rとしては資源的に豊富な軽希土類を用いるこ
とができ必ずしもSmを必要とせず或いはSmを主
体とする必要もないので原料が安価でありきわめ
て有用である。本発明によつて得られる永久磁石
材料は従来のRCo磁石材料に比べ資源的、価格的
いずれの点においても有利であり磁気特性の上か
らも一層優れたものが得られる。本発明で用いる
希土類元素RはYを含有し軽希土類及び重希土類
を包含する希土類元素であり、そのうち一種以上
を用いる。即ちこのRとしてNd、Pr、La、Ce、
Tb、Dy、Ho、Er、Eu、Sm、Gd、Pm、Tm、
Yb、Lu及びYが包含される。Rとしては軽希土
類をもつて足り、特にNd、Prが好ましい。また
通例Rとして1種をもつて足りるが実用上は2種
以上の混合物(ミツシユメタル、ジジム等)を入
手上の便宜等の理由により用いることができ、
La、Ce、Pm、Sm、Eu、Gd、Er、Tm、Yb、
Lu、Yは他のR(Nd、Pr、Dy、Ho、Tb)、特に
Nd、Prとの混合物として用いることができる。
なおRとしては純希土類元素でなくともよく工業
上入手可能な範囲で製造上不可避な不純物(他の
希土類元素、Ca、Mg、Fe、Ti、C、O等)を
含有するもので用いることが出来る。
本発明によつて製造される永久磁石材料におい
て添加元素Mは保磁力を増大させる効果をもつて
いる。保磁力の増大は磁石の安定性を増し、その
用途が拡大される。しかしMはその増大につれて
Brが低下していき、そのため最大エネルギー積
(BH)maxが減少する。(BH)maxは少し低く
なつても高い保磁力Hcが必要とされる用途は最
近ことに多くなつてきたためMを含む合金は大変
有用であるが(BH)maxは4MGOe以上の範囲
で有用である。
添加元素Mの夫々の添加によるBrへの及ぼす
効果を明らかにするためその添加量を変化させて
Brの変化を測定しハードフエライトのBr約4KG
と同等以上をその範囲とする。またハードフエラ
イトの(BH)max約4MGOeと同等以上の範囲
を考慮しMの添加量の上限はV9.5%、Mb12.5%、
Ta10.5%、Mo9.5%、W9.5%、Cr8.5%、Al9.5%
である。Mは0%を含まずまた1種もしくは2種
以上を添加することが出来る。2種以上含有する
場合には各添加元素の特性の中間の値を一般に示
し夫々の含有量は上記%の範囲内でかつその合量
が各元素に対する上記%の最大値以下とする。
前記FeCoBRM系組成の範囲内の場合、最大エ
ネルギー積(BH)maxはハードアエライト磁石
(〜4MGOe)と同等あるいはそれ以上とする。
また軽希土類元素特にNd、Prは全R中の50%以
上含有し、かつ11〜24%のR、3〜27%のB、
Co50%以下(但しCo0%除く)、添加元素Mは
V8.0%以下、Nb10.5%以下、Ta9.5%以下、
Mo7.5%以下、W7.5%以下、Cr6.5%以下、及び
Al7.5%以下であり、Mの合量は含有するMの当
該各元素のうち最大値を有するものの原子百分率
以下、残部は実質的にFeの組成範囲の場合、
(BH)maxは7MGOe以上と好ましい範囲とな
る。さらに最も好ましい範囲は軽希土類元素特に
Nd、Prを全R中の50%以上含有し、かつ12〜20
%のR、4〜24%のB、Co50%以下(但しCo0%
を除く)、添加元素MはV6.5%以下、Nb8.5%以
下、Ta8.5%以下、Mo5.5%以下、W5.5%以下、
Cr4.5%以下、及びAl5.5%以下であり、Mの合量
は含有するMの当該各元素のうち最大値を有する
ものの原子百分率以下、残部は実質的にFeの組
成範囲の場合、(BH)maxは10MGOe以上十分
可能であり、最高の最大エネルギー積は
33MGOe以上に達する。また本発明のFe−Co−
B−R−M合金はCo5%%以上で残留磁束密度
(Br)の温度係数(α)はα≦0.1%/℃となり、
温度特性が良好となり、Coを含有しないFe−B
−R合金に比較して良好な温度特性を有するのみ
ならず、Co添加により減磁曲線の角形性が改善
されるため、最大エネルギー積の向上がはかれ
る。Co25%以下において、他の磁気特性(特に
エネルギー積)は実質上悪影響を受けない。Co
が25%をこえると、(BH)maxは減少する。ま
た、CoはFeに比べて耐食性を有するので、Fe−
B−R合金にCoを添加することにより耐食性を
付与することが可能である。
本発明によつて製造されるFeCoBRM系焼結体
から成る永久磁石材料は、Fe、Co、B、R、M
の外Cu、C、S、Pを少量含有することも可能
であり(Cu3.5%以下、S2.0%以下、C4.0%以下、
P3.5%以下、但しその合量は当該各元素の最大値
以下)、製造性改善、低価格化が可能となる。更
に、Ca、Mg、O、Siの含有をも許容し、特に
Ca、Mg各4.0%以下、Si5%以下(その合量は5
%以下)が実用上好ましい。こうした元素の含有
によつても、なおハードフエライトと同程度の
Br(4kG程度)以上であり、有用である。Cu、P
は安価な原料から、Cは有機成形助剤から、Sは
製造工程から混入することがある。なお、合金粉
末の状態においては、処理工程、空気からの吸着
成分(水分、酸素等)が含まれ易いが、これらは
焼結時に除去することができる。但し、必要に応
じ工程、保存に注意する。その他、工業的製造上
不可避な不純物の存在を許容できる点で本発明は
実用的である。
以下本発明の製造方法を磁気異方性永久磁石材
料を製造する場合について更に説明する。
まず出発原料となる前記FeCoBRM系組成の合
金粉末を得る。これは通常の合金溶解・鋳造で得
た合金鋳塊を粉砕して分級、配合等により供して
もよく、あるいはCa等の還元剤を用いて酸化物
から還元法によつて得てもよいが、FeCoBRM合
金粉末の平均粒度0.3〜80μmのものを用いること
が好ましい。平均粒度80μmをこえるとすぐれた
磁石特性が得られない。平均粒度0.3μmより下で
は、微粉砕中ないしその後の製造工程において、
粉末の酸化が著しくなり、焼結後の密度が上がら
ず得られる磁石特性も低い。平均粒度40〜80μm
の範囲では磁石特性のうち保磁力がやや低い。優
れた磁石特性を得るためには合金粉末の平均粒度
として、1.0〜2.0μmが最も望ましい。
粉砕は通常の方法でよく、不活性なガス雰囲気
で行なう乾式粉砕又は有機溶媒中で行なう湿式粉
砕のいずれでもよい。湿式で行う場合、アルコー
ル系溶媒、ヘキサン、トリクロルエタン、トリク
ロルエチレン、キシレン、トルエン、フツ素系溶
媒、パラフイン系溶媒などを用いることができ
る。
次に合金粉末を成形する。成形は通例の粉末冶
金法と同様に行うことができ、加圧成形が好まし
く、異方性とするためには、磁界中でプレスす
る。例えば、合金粉末を5kOe以上の磁界中で0.5
〜3.0Ton/cm2の圧力で加圧することにより成形
体と成す。この磁界中加圧成形は粉末をそのまま
成形する方法、アセトン、トルエン等有機溶媒中
成形する方法いずれも可能である。
次に、この成形体を還元性ないし非酸化性雰囲
気中で所定温度(900〜1200℃)にて焼結する。
例えば、この成形体を10-2Torr以下の真空中な
いし、1〜760Torr、純度99.9%以上の不活性ガ
スないし還元性ガス雰囲気中で900〜1200℃の温
度範囲で0.5〜4時間焼結する。焼結温度900℃よ
り下では十分な焼結密度が得られず、高い残留磁
束密度も得られない。また1200℃より上では焼結
体が変形し結晶粒の配向がくずれるため残留磁束
密度の低下と減磁曲線の角形性が低下する。また
時間は5分以上であればよいが余り長時間になる
と量産性に問題があるので、磁石特性の再現性を
考慮すると0.5〜4時間の焼結時間が望ましい。
なお、焼結工程は、焼結の進行と共に密度が増大
し、十分な密度に達するまでの加熱工程と考えら
れる。
焼結雰囲気は本合金中の成分であるRが高温で
極めて酸化しやすいので、非酸化性雰囲気である
高真空中あるいは不活性ガス、還元性ガス雰囲気
中にて行うが、不活性ガス、還元性ガスの純度は
高い方がよい。不活性ガスを用いる場合は高い焼
結密度を得る方法として1〜760Torr未満の減圧
雰囲気中で行うことも可能である。
焼結時の昇温速度は特に規定しないが、前記湿
式プレス式の場合には有機溶媒の溶媒除去を行う
ため昇温速度40℃/min以下で昇温を行うか或い
は昇温途中で200〜800℃の温度範囲で0.5時間以
上保持して溶媒除去を行うこが望ましい。
焼結後、室温までの冷却速度は20℃/min以上
が製品のバラツキを少なくするために好ましく、
引続く熱処理(時効処理とも言う)により磁石特
性を高めるためには冷却速度として100℃/min
以上が望ましい(但し、焼結に続いて直ちに熱処
理工程に入ることもできる。)。
時効処理は真空ないし不活性ガスないし還元性
ガス雰囲気中で350℃から焼結温度以下の温度範
囲で、凡そ5分から40時間おこなう。時効処理の
雰囲気としては合金中の主成分のRが高温で酸素
或いは水分と急激に反応するので、真空の場合は
真空度10-3Torr以下、不活性ガス、還元性ガス
雰囲気の場合は雰囲気の純度99.9%以上が望まし
い。
本発明において合金の最適焼結温度は組成によ
り異なり、時効処理は本発明で得られる磁石材料
の各焼結温度以下で行う必要がある。例えば
68Fe10Co8B12Nd2W合金、
58Fe20Co5B16Nd1Al合金では時効処理の上限温
度は各々920℃、1030℃である。一般にFeに富む
あるいはBが少ない、あるいはRが少ない組成ほ
ど上限時効処理温度を高くできる。しかし、時効
処理温度が高すぎると、本発明製法において合金
の結晶粒が過剰成長し、磁石特性とりわけ保磁石
力の低下をもたらすとともに、最適時効処理時間
が極めて短時間となり製造条件の制御が困難とな
り実用的でない。また、350℃より下では時効処
理時間に極めて長時間を要するため実用的でな
く、かつ減磁曲線の角形性が低下し優れた永久磁
石にならない。本発明で得られる永久磁石材料の
結晶粒の過剰成長を起さずに優れた磁石特性を実
用的に得るには時効処理温度として450℃から800
℃が最も望ましい。時効処理は5分から40時間お
こなうが、時効処理時間が5分未満では時効処理
の効果はほとんど現れず、また得られる磁石特性
のバラツキも大きい。一方、時効処理が40時間を
こえると工業的に長時間を要しすぎるため実用的
とはいいがたい。優れた磁石特性を実用的に再現
性良く得るには時効処理時間として30分から8時
間が望ましい。
また本発明製法において磁石合金の時効処理の
手法として2段以上の多段時効処理も有効であ
り、例えば1050℃で焼結した68Fe−10Co−7B−
13Nd−1Mo−1Nb合金では1段目として820℃〜
920℃の温度範囲で30分から6時間の初段時効処
理を行つたのち、2段目以降は400〜750℃の温度
範囲で2時間から30時間の1段以上の時効処理を
行うことにより、残留磁束密度、保磁力、減磁曲
線の角形性のともに高い優れた磁石特性が得られ
る。とりわけ2段目以降の時効処理は保磁力の著
しい向上に効果がある。また時効処理の別手法と
して多段時効処理の代りに時効処理時400℃から
800℃の温度範囲を空冷・水冷等の冷却方法によ
り一定の冷却速度で冷却を行つても、同等の磁石
特性が得られるが、その際の冷却速度は0.2℃/
minから20℃/secであることが必要である。な
おこれら時効処理は焼結後そのまま行つても、焼
結後一旦室温まで冷却後再び昇温して行つても同
等の磁石特性が得られる。
また本発明の製造方法は磁気異方性永久磁石材
料のみならず等方性永久磁石材料の製造にも適用
できる。なお等方性永久磁石材料の製造方法にお
いては合金粉末を磁界中でなく成形するほか他工
程はそのまま利用することが出来る。
等方性の場合には、R10〜25%、B3〜23%、
50%以下のCo、所定%のM、残部Fe及び不可避
の不純物から成る組成において、(BH)
max2MGOe以上が得られる。等方性磁石材料は
元来異方性磁石材料の磁気特性の1/4〜1/6の低い
特性のものであるが本発明によれば、それにもか
かわらず、等方性としては極めて有用な高い特性
が得られる。
等方性の場合も、R量が増加するに従つてiHc
は増加するが、Brは最大値を経た後減少する。
かくて(BH)max2MGOe以上を満足するR量
は10%以上でかつ25%以下である。
またB量が増大するに従いiHcは増大するがBr
は最大値を経た後減少する。かくて(BH)
max2MGOe以上を得るにはB3〜23%の範囲でな
ければならない。
好ましくは軽希土類をR特にNd、Prの主成分
(全R中50原子%以上)とし12〜20%のR、5〜
18%のB、残部Feの組成で(BH)max4MGOe
以上の高い磁気特性を示す。最も好ましい範囲と
してNd、Pr等の軽希土類をRの主成分とし12〜
16%のR、6〜18%のB残部Feの組成では
(BH)maxが7MGOe以上で等方性永久磁石材料
ではかつて無い特性が得られる。
Mとしては、下記の外は異方性の場合と同じ範
囲が好ましい。(V10.5%、W8.8%以下)。いずれ
のM成分も等方性の場合、その添加量の増大と共
にBrは減少傾向を示し、Br3KG以上(等方性ハ
ードフエライトの(BH)max2MGOeのレベル
と同等以上とするため)をこの範囲内で示す。
結合剤、滑剤は、異方性の場合には、成形の際
の配向を妨げるため一般には用いられない場合が
あるが、等方性磁石の場合には、結合剤、滑剤等
を含むことによりプレス効率の改善、成形体の強
度増大等が可能である。
等方性の場合もR、B、M、Fe、Coの他に所
定範囲内でC、P、S、Cuが含有されることも
でき、C4.0%以下、P3.3%以下、S2.5%以下、
Cu3.3%以下(但しこれらの合計は、各成分のう
ち最大値以下)の範囲は製造性改善等の見地から
有用であり、更に、Ca、Mg、O、Siの含有を許
容し、Ca、Mg各4.0%以下、Si5%以下の含有
(それらの合量5%以下)が実用上好ましい。な
お、その他工業的製造上不可避な不純物の存在を
許容できる点も異方性材料におけるものと同様で
ある。
以上詳述の通り本発明の永久磁石材料の製造方
法は新規なFeCoBRM系の高保磁力・高エネルギ
ー積を備える優れた磁石特性を有し、又Rとして
Nd、Pr等の軽希土類元素を用いることにより資
源的・価格的などの点においても優れた永久磁石
材料を簡便に製造でき工業的利用性の高いもので
ある。特に、Feの一部をCoで置換することによ
つてより実用的なキユリー温度を有するものを得
ることができ、又所定元素Mを含有させると共に
所定の時効処理を施すことによつて、結晶質の
FeBR系ないしはFeCoBRM系永久磁石材料につ
いて、より一層の保磁力の向上及び滅磁曲線の角
形性の向上を実現したものである。
以下本発明の態様及び効果について、さらに実
施例に従つて説明する。但し実施例及び記載の態
様は、本発明をこれらに限定するものではない。
表1〜4は、つぎの工程によつて種々の
FeCoBRM系組成から成る永久磁石材料を作製し
た。
(1) 出発原料はFeとして純度99.9%(重量%、以
下原料純度について同じ)の電解鉄、Bとして
フエロボロン合金(19.38%B、5.32%Al、0.74
%Si、0.03%C、残部Fe)、Rとして純度99%
以上(不純物は主として他の希土類金属)を使
用。
Co純度99.9%の電解Coを使用した。Mとし
ては純度99%のTa、98%のW、99.9%のAl、
またVとしては81.2%のVを含むフオロバナジ
ウム、Nbとして67.6%のNbを含むフエロニオ
ブ、Crとして61.9%のCrを含むフエロクロムを
使用した。
(2) 磁石原料を高周波誘導を用いて溶解を行つ
た。その際ルツボとしてはアルミナルツボを用
い水冷銅鋳型中に鋳込みインゴツトを使つた。
(3) 溶解で得られたインゴツトを搗砕し−
35meshにしたのち更にボールミルにより所定
の平均粒度のものが得られるように粉砕を行つ
た。
(4) 粉末を磁界中で所定の圧力で成形した(但し
等方性磁石材料を製造する場合は磁界をかけな
いで成形した。)。
(5) 成形体は900〜1200℃の範囲内の所定の雰囲
気焼結を行い、その後所定の熱処理を行つた。
実施例 1
原子百分率組成61Fe・14Co・7B・16Nd・
2Moなる平均粒度5μmの合金粉末を10KOe磁界
中で1.5Ton/cm2の圧力で加圧成形した後、99.99
%純度の200TorrAr中で1100℃、2時間焼結し、
焼結後は冷却速度700℃/minで室温まで冷却し
た。さらに時効処理を650℃で20分、120分、240
分、3000分行い、本発明製法に係る磁石材料を得
た。磁石特性結果および本合金磁石の残留磁束密
度(Br)の温度係数α(%/℃)を比較例(焼結
後)とともに表1に示す。
The present invention relates to a method for manufacturing a novel rare earth magnet material, which is based on FeBR and contains an additive element M, in particular
This article relates to a method for manufacturing high-performance permanent magnet materials that do not necessarily require rare rare earth metals such as Sm, and whose main components are light rare earths such as Nd and Pr, which are abundant in resources and have few uses, and Fe. Permanent magnetic materials are one of the extremely important electrical and electronic materials used in a wide range of fields, from various household appliances to peripheral terminal equipment for large computers. In recent years, with the demand for smaller and more efficient electrical equipment, permanent magnet materials are required to have even higher performance. Furthermore, there is a need for magnetic materials with high coercive force in many practical applications where extremely large reverse magnetic fields are applied, such as magnetic couplings for motor generators. Representative permanent magnet materials currently in use are alnico, hard ferrite, and rare earth cobalt magnet materials. A recent permanent magnet material that satisfies high magnetic properties is a rare earth cobalt magnet material. However, rare earth cobalt magnet materials require Sm, which is a scarce resource, and its supply is unstable.
It is very expensive because it uses a large amount of Co. In order for rare earth magnet materials to be used in large quantities in a wide range of fields, it is necessary to use light rare earth metals, which are found in large amounts in ores as rare earth metals, as the main component, without containing large amounts of expensive cobalt. is necessary. As an attempt to develop such a permanent magnet material, an RFe 2 compound (where R is at least one rare earth metal) has been proposed. Clark (AE
Clark) is an amorphous material obtained by sputtering.
We found that TbFe 2 has an energy product of 29.5MGOe at 4.2〓, and when it is heat-treated at 300 to 500℃, it exhibits a coercive force of 3.4KOe and a maximum energy product of 7MGOe at room temperature. A similar study was conducted on SmFe 2 , and it was reported that SmFe 2 showed 9.2 MGOe at 77〓. However, all of these materials are thin films created by sputtering and are not magnetic materials that can be used in general speakers or motors. Also
Ribbon made by ultra-quenching PrFe alloy
It has been reported that it exhibits a high coercive force of 2.8KOe.
Furthermore, Kuhn et al. found that when an amorphous ribbon obtained by ultra-quenching (Fe.B) 0.9 Tb 0.05 La 0.05 was annealed at 627°C, the coercive force reached as high as 9KOe (Br was 5KG). However, in this case, the maximum energy product is low because the magnetization curve has poor squareness (NCKoon
Appl. Phys. Lett. 39(10) 1981, pp. 840-842). Also, L. Kabacoff et al. (Fe, B) 1-
It has been reported that ribbons made by ultra -quenching with a composition of X Pr These ultra-quenched ribbons or thin films produced by sputtering are not practical permanent magnet materials that can be used as such, and practical permanent magnet materials cannot be obtained from these ribbons or thin films. That is, it is not possible to obtain a bulk permanent magnet material having arbitrary shapes and dimensions from the FeBR-based ribbons or RFe-based thin films that have been proposed so far. Also reported so far
The magnetization curve of FeBr-based ribbons has poor squareness and is not considered a practical permanent magnet material that can compete with conventionally used magnet materials. Furthermore, ribbons produced by ultra-quench cooling and thin films produced by sputtering are essentially isotropic, and it has been virtually impossible to obtain practical permanent magnet materials with magnetic anisotropy from them. The purpose of the present invention is to eliminate the drawbacks of conventional methods, eliminate the need to use rare earths such as Sm, and
The basic objective is to obtain a new permanent magnet material that does not contain many problematic components such as Co. Furthermore, the present invention has good magnetic properties at room temperature, can be formed into any shape and practical size, has a highly square magnetization curve, and can effectively use light rare earth elements, which are abundant in resources. It is an object of the present invention to provide a manufacturing method for easily obtaining a permanent magnet material. The present inventors have previously invented an FeBR-based permanent magnet material that does not necessarily require the use of Sm or Co (Japanese Patent Application No. 145072/1982). This FeBR-based permanent magnet material is
It is based on a new compound different from the conventionally known RCo 5 and R 2 Co 17 compounds, and in particular boron (B) is used as an amorphous promoting element in the production of amorphous alloys or in powder metallurgy. It is not added as a sintering promoting element, but is an essential constituent element of the R-Fe-B compound that is magnetically stable and has a high magnetic anisotropy constant, which constitutes the substantial content of this FeBR-based permanent magnet material. (In addition, the above
It was also revealed that magnetically anisotropic sintered permanent magnets can be obtained by forming an appropriate microstructure based on FeBR-based permanent magnet materials). Furthermore, such a FeBR-based permanent magnet material can be manufactured by molding an alloy powder (composition) with a predetermined composition and an average particle size of 0.3 to 80 μm, and sintering it at 900 to 1200°C in a non-oxidizing atmosphere. He also invented the invention and filed a separate application (Patent Application 1988-88372). In order to achieve the above object, the present inventors further conducted intensive research on a method for manufacturing a crystalline permanent magnet material based on such FeBR ternary compound.
Based on the FeBR system, a part of Fe is replaced with Co, and an alloy powder of a certain composition range of the FeCoBRM system containing additive elements M (V, Nb, Ta, Mo, W, Cr, Al) is molded and sintered. The present inventors have discovered that a permanent magnet material with extremely excellent magnetic properties, especially coercive force and squareness, can be obtained by further heat-treating the permanent magnet material, leading to the present invention. That is, according to the present invention, 8 to 30% in atomic percentage
R of
is V9.5% or less, Nb12.5% or less, Ta10.5% or less, Mo9.5% or less, W9.5% or less, Cr8.5% or less, and Al9.5% or less, and contains two or more types. (If M is included, the total amount of M is less than a predetermined percentage of the maximum value of each of the M elements contained), and a portion of Fe is 50% of the total composition of the FeBRM system composition in which the remainder is substantially Fe. % or less Co
(excluding 0%) and has a FeCoBRM system composition and is sintered at 900 to 1200℃.
The above object can be achieved by a method for producing a FeCoBRM permanent magnet material, which is characterized in that heat treatment is carried out at a temperature of not less than 0.degree. C. and not more than the sintering temperature. By heat treatment, a significant increase in coercive force can be obtained for a sintered body of the same composition without deteriorating other magnetic properties. This point is extremely significant when compared with the fact that, for example, an increase in coercive force due to an increase in the rare earth element R results in a decrease in residual magnetization (see Japanese Patent Application No. 145072/1982). The presence of a predetermined amount of M further enhances the effect of increasing the coercive force by this heat treatment, and the presence of Co realizes a sufficiently high Kurie point for practical use. In addition, this FeCoBRM-based composition further contains one or more of the elements Similar post-sintering heat treatment effects can be achieved for FeCoBRM-based compositions. In this case, it is preferable to obtain such a sintered body by molding an alloy powder composition having a predetermined composition and an average particle size of 0.3 to 80 μm, particularly by sintering it in a non-oxidizing atmosphere, as in the prior application. The permanent magnet material thus obtained exhibits particularly excellent magnetic properties as a magnetically anisotropic permanent magnet material. The manufacturing method of the present invention is unique in that it can produce a magnetically anisotropic permanent magnet material, unlike the FeBR-based amorphous ribbon produced by the conventional method, but it can also produce an isotropic material. A better product can be obtained. Hereinafter, the case of manufacturing a magnetically anisotropic permanent magnet material will first be explained. In the method for producing a permanent magnet material of the present invention, FeBR
In alloy powder compositions for magnets, the temperature characteristics of the magnet material are improved by partially replacing Fe with Co, but in addition, light rare earths such as Nd and Pr, which are abundant in resources, are used as rare earth elements R. This material exhibits high magnetic properties. Generally, when Co is added to an Fe alloy, the Curie point Tc may rise or fall depending on the amount added, and it is generally difficult to predict the effect of the addition. In the present invention, it has been revealed that as a result of replacing Fe with Co, Tc gradually increases as the amount of Co substitution increases. Moreover, a similar tendency is confirmed regardless of the type of R in the magnet material composition. Even a small amount of Co substitution is effective in increasing Tc, and depending on the amount of Co substitution, an alloy with any Tc of about 310 to about 750°C can be obtained, but the amount of Co is 50% (hereinafter % is the atomic percentage in the alloy). ) The following are sufficient effects. B should be 2% or more to satisfy the coercive force of 1 kOe or more, and the residual magnetic flux density Br of hard ferrite should be approximately
In order to achieve 4kG or more, it must be 28% or less. The rare earth element R is required to be 8% or more in order to obtain a coercive force of 1 kOe or more, and is set to 30% or less because it is easily flammable, difficult to handle and manufacture industrially, and is expensive. As B, pure boron or haferoboron can be used, and a material containing Al, Si, C, etc. as an impurity can be used. As R, a light rare earth element which is abundant in resources can be used, and Sm is not necessarily required or Sm does not need to be the main component, so the raw material is inexpensive and extremely useful. The permanent magnet material obtained by the present invention is advantageous in terms of resources and cost compared to conventional RCo magnet materials, and it can also provide better magnetic properties. The rare earth element R used in the present invention is a rare earth element containing Y and including light rare earths and heavy rare earths, and one or more of them is used. That is, as this R, Nd, Pr, La, Ce,
Tb, Dy, Ho, Er, Eu, Sm, Gd, Pm, Tm,
Yb, Lu and Y are included. As R, a light rare earth element is sufficient, and Nd and Pr are particularly preferred. In addition, it is usually sufficient to have one type of R, but in practice, a mixture of two or more types (Mitsushimetal, dididim, etc.) can be used for reasons such as convenience of availability.
La, Ce, Pm, Sm, Eu, Gd, Er, Tm, Yb,
Lu, Y are other R (Nd, Pr, Dy, Ho, Tb), especially
Can be used as a mixture with Nd and Pr.
Note that R does not need to be a pure rare earth element, and may contain impurities that are unavoidable in manufacturing (other rare earth elements, Ca, Mg, Fe, Ti, C, O, etc.) within the industrially available range. I can do it. In the permanent magnet material produced according to the present invention, the additive element M has the effect of increasing the coercive force. Increasing the coercive force increases the stability of the magnet and expands its applications. However, as M increases
Br decreases, and therefore the maximum energy product (BH) max decreases. Recently, there have been many applications that require a high coercive force Hc even if the (BH)max is a little lower, so alloys containing M are very useful, but (BH)max is useful in the range of 4MGOe or more. be. In order to clarify the effect of each addition of the additive element M on Br, the amount added was varied.
Measuring the change in Br, the hard ferrite's Br is approximately 4KG.
The range is equal to or greater than. In addition, considering the range equivalent to or higher than the (BH) max of hard ferrite of approximately 4 MGOe, the upper limit of the amount of M added is V9.5%, Mb12.5%,
Ta10.5%, Mo9.5%, W9.5%, Cr8.5%, Al9.5%
It is. M does not contain 0%, and one type or two or more types can be added. When two or more kinds of additive elements are contained, the average value of the characteristics of each additive element is generally indicated, and the content of each element is within the range of the above percentages, and the total amount is not more than the maximum value of the percentages for each element. When the FeCoBRM system composition is within the above range, the maximum energy product (BH) max is equal to or greater than that of a hard aerite magnet (~4MGOe).
In addition, light rare earth elements, especially Nd and Pr, contain 50% or more of the total R, and 11 to 24% of R, 3 to 27% of B,
Co50% or less (excluding Co00%), additive element M
V8.0% or less, Nb10.5% or less, Ta9.5% or less,
Mo7.5% or less, W7.5% or less, Cr6.5% or less, and
When Al is 7.5% or less, the total amount of M is no more than the atomic percentage of the maximum value of each element of M contained, and the remainder is substantially in the composition range of Fe,
(BH)max is in a preferable range of 7MGOe or more. Furthermore, the most preferable range is light rare earth elements, especially
Contains Nd, Pr in 50% or more of the total R, and 12 to 20
% R, 4-24% B, Co 50% or less (however, Co 0%
), additive elements M are V6.5% or less, Nb8.5% or less, Ta8.5% or less, Mo5.5% or less, W5.5% or less,
Cr4.5% or less and Al5.5% or less, the total amount of M is less than the atomic percentage of the maximum value of each element of M contained, and the remainder is substantially in the composition range of Fe, (BH)max is sufficiently possible to exceed 10MGOe, and the highest maximum energy product is
Reaching 33MGOe or more. Moreover, Fe-Co- of the present invention
For B-R-M alloys, the temperature coefficient (α) of residual magnetic flux density (Br) is α≦0.1%/°C when Co is 5%% or more.
Fe-B has good temperature characteristics and does not contain Co.
Not only does it have better temperature characteristics than the -R alloy, but the addition of Co improves the squareness of the demagnetization curve, leading to an improvement in the maximum energy product. Below 25% Co, other magnetic properties (especially the energy product) are not substantially adversely affected. Co
When exceeds 25%, (BH)max decreases. In addition, since Co has higher corrosion resistance than Fe,
Corrosion resistance can be imparted to the BR alloy by adding Co. Permanent magnet materials made of FeCoBRM-based sintered bodies manufactured by the present invention include Fe, Co, B, R, M
It is also possible to contain small amounts of Cu, C, S, and P (Cu3.5% or less, S2.0% or less, C4.0% or less,
P3.5% or less (however, the total amount is less than the maximum value of each element), improving manufacturability and lowering prices. Furthermore, the inclusion of Ca, Mg, O, and Si is also allowed, especially
Ca, Mg each 4.0% or less, Si 5% or less (the total amount is 5% or less)
% or less) is practically preferred. Even with the inclusion of these elements, it is still comparable to hard ferrite.
It is more than Br (about 4kG) and is useful. Cu, P
may be mixed in from cheap raw materials, C may be mixed in from organic molding aids, and S may be mixed in during the manufacturing process. Note that in the state of alloy powder, adsorbed components (moisture, oxygen, etc.) from the air during processing are likely to be included, but these can be removed during sintering. However, care should be taken in processing and storage as necessary. In addition, the present invention is practical in that it can tolerate the presence of impurities that are inevitable in industrial production. The manufacturing method of the present invention will be further explained below regarding the case of manufacturing a magnetically anisotropic permanent magnet material. First, an alloy powder having the aforementioned FeCoBRM composition is obtained as a starting material. This may be obtained by crushing an alloy ingot obtained by ordinary alloy melting and casting, classification, blending, etc., or it may be obtained by a reduction method from an oxide using a reducing agent such as Ca. It is preferable to use FeCoBRM alloy powder having an average particle size of 0.3 to 80 μm. If the average particle size exceeds 80 μm, excellent magnetic properties cannot be obtained. If the average particle size is less than 0.3 μm, during pulverization or the subsequent manufacturing process,
The oxidation of the powder becomes significant, and the density after sintering does not increase, resulting in poor magnetic properties. Average particle size 40~80μm
In the range of , the coercive force among the magnetic characteristics is somewhat low. In order to obtain excellent magnetic properties, the average particle size of the alloy powder is most preferably 1.0 to 2.0 μm. The pulverization may be carried out by a conventional method, and may be either dry pulverization carried out in an inert gas atmosphere or wet pulverization carried out in an organic solvent. When carrying out in a wet manner, alcohol-based solvents, hexane, trichloroethane, trichloroethylene, xylene, toluene, fluorine-based solvents, paraffin-based solvents, etc. can be used. Next, the alloy powder is shaped. The molding can be carried out in the same manner as the usual powder metallurgy method, preferably pressure molding, and in order to obtain anisotropy, pressing in a magnetic field. For example, alloy powder is 0.5 kOe or more in a magnetic field of 5 kOe or more.
A molded body is formed by applying a pressure of ~3.0Ton/cm 2 . This pressure molding in a magnetic field can be performed either by molding the powder as it is or by molding it in an organic solvent such as acetone or toluene. Next, this molded body is sintered at a predetermined temperature (900 to 1200°C) in a reducing or non-oxidizing atmosphere.
For example, this compact is sintered for 0.5 to 4 hours at a temperature range of 900 to 1200°C in a vacuum of 10 -2 Torr or less or in an inert gas or reducing gas atmosphere of 1 to 760 Torr and a purity of 99.9% or more. . If the sintering temperature is lower than 900°C, sufficient sintered density and high residual magnetic flux density cannot be obtained. Moreover, above 1200°C, the sintered body is deformed and the orientation of crystal grains is disrupted, resulting in a decrease in residual magnetic flux density and a decrease in the squareness of the demagnetization curve. Further, the sintering time may be 5 minutes or more, but if it is too long, there will be a problem in mass productivity, so in consideration of the reproducibility of the magnetic properties, a sintering time of 0.5 to 4 hours is desirable.
Note that the sintering process is considered to be a heating process in which the density increases as the sintering progresses and reaches a sufficient density. The sintering atmosphere is a non-oxidizing atmosphere, such as a high vacuum or an inert gas or reducing gas atmosphere, since R, which is a component in this alloy, is extremely susceptible to oxidation at high temperatures. The higher the purity of the sexual gas, the better. When using an inert gas, it is also possible to carry out the sintering in a reduced pressure atmosphere of 1 to less than 760 Torr as a method of obtaining high sintering density. The temperature increase rate during sintering is not particularly specified, but in the case of the wet press method, in order to remove the organic solvent, the temperature is increased at a rate of 40℃/min or less, or the temperature is increased from 200℃ to 200℃ during the temperature increase. It is desirable to remove the solvent by holding it in a temperature range of 800°C for 0.5 hours or more. After sintering, the cooling rate to room temperature is preferably 20°C/min or more to reduce product variation.
In order to improve the magnetic properties through subsequent heat treatment (also called aging treatment), the cooling rate must be 100℃/min.
The above is desirable (however, it is also possible to start the heat treatment process immediately after sintering). The aging treatment is carried out in a vacuum, inert gas, or reducing gas atmosphere at a temperature range from 350°C to below the sintering temperature for about 5 minutes to 40 hours. The aging treatment atmosphere should be a vacuum of 10 -3 Torr or less, or an inert gas or reducing gas atmosphere, since R, the main component in the alloy, reacts rapidly with oxygen or moisture at high temperatures. A purity of 99.9% or higher is desirable. In the present invention, the optimum sintering temperature of the alloy varies depending on the composition, and the aging treatment must be performed at a temperature below each sintering temperature of the magnet material obtained in the present invention. for example
68Fe10Co8B12Nd2W alloy,
For 58Fe20Co5B16Nd1Al alloy, the upper limit temperature for aging treatment is 920℃ and 1030℃, respectively. In general, the upper limit aging temperature can be increased as the composition is richer in Fe, less B, or less R. However, if the aging treatment temperature is too high, the crystal grains of the alloy will grow excessively in the manufacturing method of the present invention, leading to a decrease in magnetic properties, especially coercive force, and the optimum aging treatment time will be extremely short, making it difficult to control manufacturing conditions. Therefore, it is not practical. Further, if the temperature is lower than 350°C, the aging treatment time will take an extremely long time, which is impractical, and the squareness of the demagnetization curve will deteriorate, making it impossible to obtain an excellent permanent magnet. In order to practically obtain excellent magnetic properties without causing excessive growth of crystal grains in the permanent magnet material obtained by the present invention, the aging treatment temperature must be 450°C to 800°C.
°C is most desirable. The aging treatment is performed for 5 minutes to 40 hours, but if the aging treatment time is less than 5 minutes, the effect of the aging treatment will hardly be apparent, and the obtained magnet properties will vary widely. On the other hand, if the aging treatment exceeds 40 hours, it is difficult to say that it is practical because it takes too long for industrial purposes. In order to practically obtain excellent magnetic properties with good reproducibility, the aging treatment time is preferably 30 minutes to 8 hours. In addition, in the manufacturing method of the present invention, multi-stage aging treatment of two or more stages is also effective as a method for aging the magnetic alloy. For example, 68Fe-10Co-7B-
For 13Nd−1Mo−1Nb alloy, the first stage is 820℃~
After performing the first stage aging treatment in the temperature range of 920℃ for 30 minutes to 6 hours, the second stage and subsequent stages are subjected to one or more stages of aging treatment in the temperature range of 400 to 750℃ for 2 hours to 30 hours. Excellent magnetic properties with high magnetic flux density, coercive force, and squareness of the demagnetization curve can be obtained. In particular, the second and subsequent aging treatments are effective in significantly improving coercive force. In addition, as another method of aging treatment, instead of multi-stage aging treatment,
Even if the temperature range of 800℃ is cooled at a constant cooling rate using air cooling, water cooling, etc., the same magnetic characteristics can be obtained, but the cooling rate in that case is 0.2℃/
It is necessary that the temperature is from min to 20°C/sec. Note that the same magnetic characteristics can be obtained even if these aging treatments are performed as is after sintering, or if the temperature is raised again after cooling to room temperature after sintering. Further, the manufacturing method of the present invention can be applied not only to the manufacturing of magnetically anisotropic permanent magnet materials but also to the manufacturing of isotropic permanent magnet materials. In addition, in the method for producing an isotropic permanent magnet material, the alloy powder is molded without being placed in a magnetic field, and other steps can be used as is. For isotropic case, R10~25%, B3~23%,
In a composition consisting of 50% or less Co, a certain % M, the balance Fe and unavoidable impurities, (BH)
You can get more than max2MGOe. Isotropic magnet materials originally have low magnetic properties, 1/4 to 1/6 of the magnetic properties of anisotropic magnet materials, but according to the present invention, they are nevertheless extremely useful as isotropic materials. High characteristics can be obtained. Even in the case of isotropy, as the amount of R increases, iHc
increases, but Br decreases after reaching its maximum value.
Thus, the amount of R that satisfies (BH)max2MGOe or more is 10% or more and 25% or less. Also, as the amount of B increases, iHc increases, but Br
decreases after reaching its maximum value. Thus (BH)
Must be in the range of B3-23% to get max2MGOe or higher. Preferably, light rare earths are the main components of R, especially Nd, Pr (at least 50 atomic % of the total R), and 12 to 20% R, 5 to
With a composition of 18% B, balance Fe (BH) max4MGOe
It exhibits high magnetic properties as described above. The most preferable range is from 12 to 12, with light rare earths such as Nd and Pr as the main components of R.
With a composition of 16% R, 6 to 18% B balance Fe, (BH)max is 7MGOe or more, and properties unprecedented in isotropic permanent magnet materials can be obtained. M is preferably within the same range as in the case of anisotropy except for the following. (V10.5%, W8.8% or less). When any M component is isotropic, Br shows a decreasing tendency as the amount added increases, and Br3KG or more (to be equal to or higher than the level of (BH)max2MGOe of isotropic hard ferrite) is within this range. Indicated by Binders and lubricants are generally not used in the case of anisotropic magnets because they interfere with the orientation during molding, but in the case of isotropic magnets, by including binders and lubricants, It is possible to improve the press efficiency and increase the strength of the molded product. In the case of isotropy, in addition to R, B, M, Fe, and Co, C, P, S, and Cu can also be contained within a specified range, such as C4.0% or less, P3.3% or less, and S2. .5% or less,
A range of Cu3.3% or less (however, the total of these is less than the maximum value of each component) is useful from the standpoint of improving manufacturability, etc. Furthermore, the content of Ca, Mg, O, and Si is allowed, and Ca , Mg, each 4.0% or less, and Si 5% or less (the total amount of these is 5% or less) is practically preferable. Note that the presence of other impurities that are unavoidable in industrial production can be tolerated, as in the case of anisotropic materials. As detailed above, the method for manufacturing the permanent magnet material of the present invention has excellent magnetic properties with high coercive force and high energy product of the novel FeCoBRM system, and as R
By using light rare earth elements such as Nd and Pr, it is possible to easily produce permanent magnet materials that are excellent in terms of resources and cost, and have high industrial applicability. In particular, by substituting a part of Fe with Co, it is possible to obtain a crystal with a more practical Curie temperature, and by incorporating a certain element M and subjecting it to a certain aging treatment, it is possible to obtain a crystal with a more practical Curie temperature. quality
This material achieves further improvements in coercive force and squareness of the demagnetization curve for FeBR-based or FeCoBRM-based permanent magnet materials. The aspects and effects of the present invention will be further explained below with reference to Examples. However, the present invention is not limited to the examples and described aspects. Tables 1 to 4 show various results depending on the following steps.
A permanent magnet material consisting of FeCoBRM composition was fabricated. (1) The starting materials are electrolytic iron with a purity of 99.9% (weight%, the same applies to raw material purity below) as Fe, and feroboron alloy (19.38% B, 5.32% Al, 0.74% B) as B.
%Si, 0.03%C, balance Fe), purity 99% as R
The above (impurities are mainly other rare earth metals) are used. Electrolytic Co with a Co purity of 99.9% was used. M is Ta with a purity of 99%, W with a purity of 98%, Al with a purity of 99.9%,
Fluorovanadium containing 81.2% V was used as V, ferronniobium containing 67.6% Nb was used as Nb, and ferrochrome containing 61.9% Cr was used as Cr. (2) Magnet raw materials were melted using high-frequency induction. At that time, an aluminum crucible was used as the crucible, and an ingot cast into a water-cooled copper mold was used. (3) Crush the ingot obtained by melting.
After making the powder into 35 mesh, it was further pulverized using a ball mill to obtain a predetermined average particle size. (4) The powder was molded under a predetermined pressure in a magnetic field (however, when manufacturing an isotropic magnet material, molding was performed without applying a magnetic field). (5) The compact was sintered in a predetermined atmosphere within the range of 900 to 1200°C, and then subjected to a predetermined heat treatment. Example 1 Atomic percentage composition 61Fe・14Co・7B・16Nd・
After pressing 2Mo alloy powder with an average particle size of 5 μm in a 10KOe magnetic field at a pressure of 1.5Ton/ cm2 , it becomes 99.99
Sintered at 1100℃ for 2 hours in 200TorrAr with % purity,
After sintering, it was cooled to room temperature at a cooling rate of 700°C/min. Furthermore, aging treatment was performed at 650℃ for 20 minutes, 120 minutes, and 240 minutes.
The magnet material according to the manufacturing method of the present invention was obtained by carrying out the experiment for 3,000 minutes. The magnet characteristic results and the temperature coefficient α (%/°C) of the residual magnetic flux density (Br) of this alloy magnet are shown in Table 1 together with a comparative example (after sintering).
【表】
実施例 2
原子百分率組成55Fe・150Co・12B・14Nd・
2Y・2Nd、平均粒度3μmの合金粉末を15bOe磁
界中で1.0Ton/cm2の圧力で加圧成形した後、
99.999%純度の500TorrAr中で1180℃、2時間焼
結し、焼結後は冷却速度450℃/minで室温まで
冷却した。さらに2×10-5Torr真空中にて時効
処理を表2に示す各温度にて3時間行い、本発明
製法による磁石材料を得た。磁石特性結果および
残留磁束密度(Br)の温度係数α(%/℃)を比
較例(焼結後等)とともに表2に示す。[Table] Example 2 Atomic percentage composition 55Fe・150Co・12B・14Nd・
After pressing 2Y/2Nd alloy powder with an average particle size of 3μm in a 15bOe magnetic field at a pressure of 1.0Ton/ cm2 ,
Sintering was performed at 1180°C for 2 hours in 500 TorrAr with a purity of 99.999%, and after sintering, the material was cooled to room temperature at a cooling rate of 450°C/min. Furthermore, aging treatment was performed in a vacuum of 2×10 −5 Torr at each temperature shown in Table 2 for 3 hours to obtain a magnet material according to the production method of the present invention. The magnet characteristic results and the temperature coefficient α (%/°C) of the residual magnetic flux density (Br) are shown in Table 2 together with comparative examples (after sintering, etc.).
【表】【table】
【表】
実施例 3
平均粒度2〜15μm、表3に示す原子百分率組
成を有するFeCoBRM合金粉末を10kOe磁界中で
1.8Ton/cm2の圧力で加圧成形した後、99.999%純
度の250TorrAr中で1080℃、2時間焼結し、焼
結後は冷却速度700℃/minで室温まで急速冷却
した。さらに600TorrのAr中にて時効処理を700
℃で4時間行い、本発明製法による磁石材料を得
た。磁石特性およびBrの温度係数α(%/℃)の
値をCoを含有しない比較例とともに表3に示す。[Table] Example 3 FeCoBRM alloy powder having an average particle size of 2 to 15 μm and the atomic percentage composition shown in Table 3 was prepared in a 10 kOe magnetic field.
After pressure molding at a pressure of 1.8Ton/cm 2 , it was sintered at 1080°C for 2 hours in 250TorrAr with a purity of 99.999%, and after sintering, it was rapidly cooled to room temperature at a cooling rate of 700°C/min. Furthermore, aging treatment is performed for 700 hours in Ar of 600 Torr.
C. for 4 hours to obtain a magnet material according to the manufacturing method of the present invention. The magnetic properties and the temperature coefficient α (%/°C) of Br are shown in Table 3 along with a comparative example that does not contain Co.
【表】
実施例 4
平均粒度1〜10μmを有する下記原子百分率組
成のFeCoBRM合金粉末を無磁界中で1.0Ton/
cm2の圧力で加圧成形した後、99.9%純度の
150TorrAr中で1020℃、1時間焼結し、焼結後
は冷却速度550℃/minで室温まで急速冷却した。
さらに650TorrAr中にて時効処理を600℃で4時
間行い、本発明製法による磁石材料を得た。磁石
特性の結果を時効処理なしの焼結後の試料(比較
例)とともに表4に示す。[Table] Example 4 FeCoBRM alloy powder having the following atomic percentage composition and having an average particle size of 1 to 10 μm was heated at 1.0 Ton/min in a non-magnetic field.
After pressure molding with a pressure of cm2 , 99.9% purity
Sintering was performed at 1020°C for 1 hour in 150TorrAr, and after sintering, the material was rapidly cooled to room temperature at a cooling rate of 550°C/min.
Further, aging treatment was performed at 600° C. for 4 hours in 650 TorrAr to obtain a magnet material according to the manufacturing method of the present invention. The results of the magnetic properties are shown in Table 4 together with the sample after sintering without aging treatment (comparative example).
Claims (1)
含する希土類元素の少なくとも1種)、2〜28%
のB、所定%以下の添加元素Mの1種又は2種以
上(但しM0%を除き、Mは V9.5%以下、 Nb12.5%以下、 Ta10.5%以下、 Mo9.5%以下、 W9.5%以下、 Cr8.5%以下、 及びAl9.5%以下であり、 2種以上のMを含む場合M合量は含有するMの
当該各元素のうち最大値を有するものの所定%以
下)、及び残部実質上FeからなるFeBRM系組成
のうちFeの一部を全組成に対して50%以下のCo
(0%を除く)で置換してなるFeCoBRM系組成
を有し、900〜1200℃で焼結してなる焼結体を350
℃以上当該焼結温度以下の温度で熱処理すること
を特徴とする永久磁石材料の製造方法。 2 前記焼結体は、前記FeCoBRM系組成を有
し、平均粒度0.3〜80μmの合金粉末組成物を成
形、焼結して得られる特許請求の範囲第1項記載
の永久磁石材料の製造方法。 3 原子百分率で8〜30%のR(但しRはYを包
含する希土類元素の少なくとも1種)、2〜28%
のB、所定%以下の添加元素Mの1種又は2種以
上(但しM0%を除き、Mは V9.5%以下、 Mb12.5%以下、 Ta10.5%以下、 Mo9.5%以下、 W9.5%以下、 Cr8.5%以下、 及びAl9.5%以下であり、 2種以上のMを含む場合M合量は含有するMの
当該各元素のうち最大値を有するものの所定%以
下)、所定%以下の元素Xの一種又は二種以上
(所定%以下の元素XはCu3.5%以下、S2.0%以
下、C4.0%以下及びP3.5%以下であり、Xが二種
以上のときX合量は当該各元素のうち最大所定%
を有するものの当該所定%以下)、及び残部実質
上FeからなるFeBRM系組成のうちFeの一部を
全組成に対して50%以下のCo(0%を除く)で置
換してなるFeCoBRM系組成を有し、900〜1200
℃で焼結してなる焼結体を350℃以上当該焼結温
度以下の温度で熱処理することを特徴とする永久
磁石材料の製造方法。[Claims] 1. 8 to 30% R (wherein R is at least one rare earth element including Y), 2 to 28% in atomic percentage
of B, one or more of the additive elements M in a specified percentage or less (excluding M0%, M is V9.5% or less, Nb12.5% or less, Ta10.5% or less, Mo9.5% or less, W is 9.5% or less, Cr is 8.5% or less, and Al is 9.5% or less, and if two or more types of M are included, the total M content is less than or equal to the specified % of the maximum value of each M element contained. ), and of the FeBRM system composition where the remainder is essentially Fe, a portion of the Fe is replaced by Co, which accounts for less than 50% of the total composition.
(excluding 0%) and has a FeCoBRM system composition and is sintered at 900 to 1200℃.
A method for producing a permanent magnet material, characterized in that heat treatment is performed at a temperature of not less than 0.degree. C. and not more than the sintering temperature. 2. The method of manufacturing a permanent magnet material according to claim 1, wherein the sintered body is obtained by molding and sintering an alloy powder composition having the FeCoBRM composition and having an average particle size of 0.3 to 80 μm. 3 8 to 30% R in atomic percentage (however, R is at least one rare earth element including Y), 2 to 28%
of B, one or more types of additive elements M at a specified percentage or less (excluding M0%, M is V9.5% or less, Mb12.5% or less, Ta10.5% or less, Mo9.5% or less, W is 9.5% or less, Cr is 8.5% or less, and Al is 9.5% or less, and if two or more types of M are included, the total M content is less than or equal to the specified % of the maximum value of each M element contained. ), one or more types of element When there are two or more types, the combined amount of X is the maximum specified percentage of each element.
(not more than the specified percentage), and a FeCoBRM composition in which part of the Fe is replaced with 50% or less of Co (excluding 0%) in the entire composition of the FeBRM composition in which the remainder substantially consists of Fe. 900~1200
A method for producing a permanent magnet material, which comprises heat-treating a sintered body obtained by sintering at ℃ at a temperature of 350℃ or higher and lower than the sintering temperature.
Priority Applications (7)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP58092238A JPS59218705A (en) | 1983-05-27 | 1983-05-27 | Permanent magnet material and manufacture thereof |
| US06/532,471 US4601875A (en) | 1983-05-25 | 1983-09-15 | Process for producing magnetic materials |
| CA000436891A CA1287509C (en) | 1983-05-25 | 1983-09-16 | Process for producing magnetic materials |
| DE8383109508T DE3378707D1 (en) | 1983-05-25 | 1983-09-23 | Process for producing of a permanent magnet |
| EP83109508A EP0126802B2 (en) | 1983-05-25 | 1983-09-23 | Process for producing of a permanent magnet |
| SG594/90A SG59490G (en) | 1983-05-25 | 1990-07-18 | Process for producing of a permanent magnet |
| HK753/90A HK75390A (en) | 1983-05-25 | 1990-09-20 | Process for producing of a permanent magnet |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP58092238A JPS59218705A (en) | 1983-05-27 | 1983-05-27 | Permanent magnet material and manufacture thereof |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS59218705A JPS59218705A (en) | 1984-12-10 |
| JPH0320048B2 true JPH0320048B2 (en) | 1991-03-18 |
Family
ID=14048852
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP58092238A Granted JPS59218705A (en) | 1983-05-25 | 1983-05-27 | Permanent magnet material and manufacture thereof |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS59218705A (en) |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS61113736A (en) * | 1984-11-09 | 1986-05-31 | Agency Of Ind Science & Technol | Manufacture of sintered magnet of rare earth-transition metal compound |
| JP2642619B2 (en) * | 1985-03-13 | 1997-08-20 | 日立金属株式会社 | Manufacturing method of permanent magnet |
| JPS6342910A (en) * | 1986-08-07 | 1988-02-24 | Toho Rayon Co Ltd | Production of acrylonitrile yarn bundle for manufacturing carbon yarn |
| JPS63119205A (en) * | 1986-11-06 | 1988-05-23 | Shin Etsu Chem Co Ltd | sintered permanent magnet |
| JP4742228B2 (en) * | 2006-03-17 | 2011-08-10 | 日産自動車株式会社 | Alloy strip for rare earth magnet and manufacturing method, alloy for rare earth magnet |
-
1983
- 1983-05-27 JP JP58092238A patent/JPS59218705A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS59218705A (en) | 1984-12-10 |
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